AD 76-15-03

Airworthiness directive · Main Rotor Blade Tension-Torsion Straps · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 1 more

Effective
July 29, 1976
Models
206A, 206A-1 (OH-58A), 206B, 206B-1
Data sheet
TCDSH2SW
Registered aircraft
861 matched by model
Product
Aircraft · Rotorcraft
Amendment
39-2675

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

76-15-03 BELL: Amendment 39-2675. Applies to Bell Models 206A, 206B, 206A-1, and 206B-1 helicopters, equipped with main rotor blade tension-torsion straps, P/N 206-010-105-3, certificated in all categories.

Compliance required as indicated.

To detect straps with inadequate torsional resistance or stiffness and to remove certain straps possibly made from certain spools of wire from further service, comply with the following.

(a) Within the next 25 hours' time in service after the effective date of this AD, accomplish the following, unless previously accomplished:

(1) Determine the serial number of each strap and remove from service straps having serial numbers 15432 through 15472 in accordance with the pertinent model maintenance manual or an FAA approved equivalent.

(2) Conduct the inspections noted in paragraph II of Bell Helicopter Company Service Bulletin No. 206-76-4, Revision A dated May 11, 1976, or a later approved revision and remove those strapswith unacceptable rotation (inadequate torsional resistance) before further flight.

(b) Prior to installing replacement straps or replacement hub assemblies, determine that paragraphs (a)(1) and (a)(2) of this AD have been accomplished. Install replacement straps in accordance with the pertinent model maintenance manual or an FAA approved equivalent.

(c) The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to the Service Manager, Bell Helicopter Company, P. O. Box 482, Fort Worth, Texas 76101. These documents may also be examined at the Office of the Regional Counsel, Southwest Region, FAA, 4400 Blue Mound Road, Fort Worth, Texas, and at FAA Headquarters, 800 Independence Avenue, S.W., Washington, D.C. A historical file on this AD, which includes the incorporated material in full, is maintained by the FAA at its headquarters in Washington, D.C., and at the Southwest Regional Office in Fort Worth, Texas.

This amendment becomes effective July 29, 1976.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 861

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Bell822 aircraft
  • Bell Helicopter Textron29 aircraft
  • Bell Helicopter Textron Canada10 aircraft
By year built
19542009
Registered aircraft by year built: 707 aircraft
19541
19661
19675
196816
196912
19707
197115
197222
197325
197439
197538
197634
197728
197840
197948
198045
198152
198227
19835
19847
19855
19865
19874
198811
198914
19907
19919
19926
199324
199438
199547
19964
19976
19985
19994
20006
200113
20027
20033
20042
20055
20066
20075
20083
20091

154 with no year recorded

By model

Aircraft

See all 861 aircraft